R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-31-44Page 437 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 32-31-44-400-003
Installation of the Uplock Assembly 2509GM (2510GM) with A/C on Jacks
1. Reason for the Job
__________________
This task is applicaple if in the installation procedure the setting tool-uplock is used. This is necessary, if the uplock needs new adjustment.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific container No specific hydraulic cart No specific warning notices No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
(15.00 to 150.00 lbf.ft) 98DNSA20208060 2 RIGGING PIN 98D32104018000 1 SETTING TOOL-UPLOCK
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 07-010 D DA-4-653-91 LACQUER OBSOLETE USE 16-047 (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-31-44Page 438 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
3 cotter pin
15 cotter pin
28 cotter pin
32 cotter pin
38 cotter pin
D. Referenced Information
32-31-03 22 -12032-31-03 22 -260A32-31-03 22 -260A32-31-03 22 -06032-33-03 01 -170
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump
20-28-00-912-004 Electrical Bonding of Components With Conductive
Bolts and Screws and Bonding Straps in the Fuselage
and in the Wings (this does not include the tanks)-
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power
29-00-00-910-002 Safety Procedures of the Hydraulic System
29-10-00-864-001 Depressurize the Green Hydraulic System
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU)
29-23-00-860-002 Connection of the Isolation Coupling of the Power
Transfer Unit (PTU)
32-00-00-860-001 Flight Configuration Precautions with Electrical
Power
32-00-00-860-002 Ground Configuration after Flight Configuration with
Electrical Power
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
32-31-00-720-002 Functional Test of the Normal Extension and
Retraction of the Landing Gear
32-33-00-720-001 Functional Check of Free-Fall Extension
51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound
32-31-44-991-001 Fig. 401
32-31-44-991-005 Fig. 405
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3. Job Set-up
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Subtask 32-31-44-860-057
A. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft is on jacks
(2)
Make sure that the PTU isolation coupling is disconnected (Ref. TASK 29-23-00-860-001).
(3)
Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002)
(4)
Make sure that the flight configuration precautions are obeyed (Ref. TASK 32-00-00-860-001).
(5)
Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-10-00-864-001).
(6)
Make sure that the reservoir of the Green hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).
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